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タイトル
和文: 
英文:Thermodynamic Effect on Backflow Vortex Cavitation 
著者
和文: 角田篤洋, 伊藤優, 谷直樹, 長崎孝夫.  
英文: Atsuhiro Tsunoda, Yu Ito, Naoki TANI, TAKAO NAGASAKI.  
言語 English 
掲載誌/書名
和文: 
英文:Proceedings of AIAA SciTech 2015 
巻, 号, ページ        
出版年月 2015年1月5日 
出版者
和文: 
英文:The American Institute of Aeronautics and Astronautics 
会議名称
和文: 
英文:53rd AIAA Aerospace Sciences Meeting 
開催地
和文: 
英文:Kissimmee, Florida 
DOI https://doi.org/10.2514/6.2015-0471
アブストラクト An experimental apparatus was developed to visualize a rotating inducer with speeds of 0 to 8000 rpm. The transparent casing outside the inducer was made of quartz glass, so that tip clearance remained almost constant. All other key parts were chosen based on their suitability for both cryogen and water. Backflow vortex cavitation on a rotating inducer was observed in either liquid nitrogen or water. Consequently, the orbital rotational rate, the orbital rotational diameter, and the diameter of each backflow vortex cavitation should be sorted by head coefficient. Further, thermodynamic effects were observed for the diameter of each backflow vortex cavitation.

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